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WO2010116529A1 - Tank and fabrication method thereof - Google Patents

Tank and fabrication method thereof Download PDF

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Publication number
WO2010116529A1
WO2010116529A1 PCT/JP2009/057358 JP2009057358W WO2010116529A1 WO 2010116529 A1 WO2010116529 A1 WO 2010116529A1 JP 2009057358 W JP2009057358 W JP 2009057358W WO 2010116529 A1 WO2010116529 A1 WO 2010116529A1
Authority
WO
WIPO (PCT)
Prior art keywords
layer
tank
fiber
helical
winding
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/JP2009/057358
Other languages
French (fr)
Japanese (ja)
Inventor
弘和 大坪
基弘 水野
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Toyota Motor Corp
Original Assignee
Toyota Motor Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Toyota Motor Corp filed Critical Toyota Motor Corp
Priority to PCT/JP2009/057358 priority Critical patent/WO2010116529A1/en
Publication of WO2010116529A1 publication Critical patent/WO2010116529A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C1/00Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
    • F17C1/16Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of plastics materials
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C1/00Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
    • F17C1/02Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge involving reinforcing arrangements
    • F17C1/04Protecting sheathings
    • F17C1/06Protecting sheathings built-up from wound-on bands or filamentary material, e.g. wires
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01Shape
    • F17C2201/0104Shape cylindrical
    • F17C2201/0109Shape cylindrical with exteriorly curved end-piece
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602Wall structures; Special features thereof
    • F17C2203/0604Liners
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602Wall structures; Special features thereof
    • F17C2203/0612Wall structures
    • F17C2203/0614Single wall
    • F17C2203/0619Single wall with two layers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634Materials for walls or layers thereof
    • F17C2203/0658Synthetics
    • F17C2203/0663Synthetics in form of fibers or filaments
    • F17C2203/0665Synthetics in form of fibers or filaments radially wound
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634Materials for walls or layers thereof
    • F17C2203/0658Synthetics
    • F17C2203/0663Synthetics in form of fibers or filaments
    • F17C2203/067Synthetics in form of fibers or filaments helically wound
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2205/00Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/03Fluid connections, filters, valves, closure means or other attachments
    • F17C2205/0302Fittings, valves, filters, or components in connection with the gas storage device
    • F17C2205/0305Bosses, e.g. boss collars
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2205/00Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/03Fluid connections, filters, valves, closure means or other attachments
    • F17C2205/0388Arrangement of valves, regulators, filters
    • F17C2205/0394Arrangement of valves, regulators, filters in direct contact with the pressure vessel
    • F17C2205/0397Arrangement of valves, regulators, filters in direct contact with the pressure vessel on both sides of the pressure vessel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2209/00Vessel construction, in particular methods of manufacturing
    • F17C2209/21Shaping processes
    • F17C2209/2154Winding

Definitions

  • the present invention relates to a tank and a manufacturing method thereof. More specifically, the present invention relates to an improvement in the structure of a tank filled with hydrogen gas or the like at a high pressure.
  • a tank used for storing hydrogen gas or the like As a tank used for storing hydrogen gas or the like, a tank that is provided with an FRP layer in which a plurality of hoop layers and a helical layer are laminated on the outer periphery of the liner and is reduced in weight is used (for example, see Patent Document 1). ).
  • the liner functions as a member that prevents permeation of hydrogen gas and the like and stores it in an airtight manner
  • the FRP layer functions as a member that provides strength to withstand high internal pressure.
  • the hoop layer forming the FRP layer is a layer formed by winding a fiber (for example, carbon fiber) by hoop winding (a method of winding the fiber around the tank axis in the tank body portion). (It is substantially parallel to the tank axis and is wound up to the tank dome.) (See FIG. 2). Further, helical winding can be performed in different manners such as high angle helical winding and low angle helical winding by changing the winding angle with respect to the tank axis. When forming the FRP layer in this manner, how the fibers are wound is an important factor for improving the efficiency of strength expression by the FRP layer.
  • a circumferential fiber layer (hoop layer, high-angle helical layer) and an axial fiber layer (low-angle helical layer) are alternately wound. is there.
  • the fiber coverage is 100% or more.
  • the fiber coverage here refers to the ratio of the one-sided surface area of the fiber wound around the layer to the surface area of the tank body part (surface area of the fiber wound around the layer / body part surface area). It can be determined by x100. The coverage when the entire surface area of the body portion is covered with the minimum necessary fibers is 100%.
  • the tank is a sealed container in which, for example, both ends of a cylindrical main body part are formed in a substantially hemispherical dome part.
  • a substantially hemispherical part is a dome part
  • a cylindrical body part is a body part ( Or straight part).
  • an object of the present invention is to provide a tank that suppresses an increase in the size or mass of the tank due to a fiber layer such as a helical layer, and a manufacturing method thereof.
  • a general method is to form a fiber layer by winding a circumferential fiber layer (hoop layer, high-angle helical layer) and an axial fiber layer (low-angle helical layer) around the liner.
  • a circumferential fiber layer hover layer, high-angle helical layer
  • an axial fiber layer low-angle helical layer
  • the fiber layers are laminated in this way, it is considered that the outer fiber layers are more difficult to fully exhibit the strength of the fibers.
  • the fibers are wound without sufficiently exerting the strength, the amount of fibers is large for the strength, and the tank may have a large physique.
  • the fiber wound on the outer layer side can contribute to an increase in the tank diameter if it is wound many times even though the contribution to the strength is small.
  • the present inventor who has further studied based on such a situation has come to obtain new knowledge that leads to the solution of such problems.
  • the present invention is based on such knowledge, and is a tank having a liner, and a FRP layer composed of a hoop layer and a helical layer formed by winding fibers on the outer periphery of the liner, and depends on the fibers of the helical layer.
  • the cover rate of the tank body is lower on the outer layer side than on the inner layer side of the FRP layer.
  • the layer located on the outer layer side of the tank and the helical layer have a small contribution in terms of fiber strength with respect to the cylindrical body part (tank body part) of the tank. That is, the fiber layer located on the outer layer side or the helical layer at a lower angle is more difficult to exert the strength of the fiber and to tightly wind the body portion of the tank.
  • the helical layer in the cylindrical body part it is possible to exert a fiber strength greater than that of the helical layer. Nevertheless, the uniform coverage by the fibers as in the conventional method is disadvantageous in that it is difficult to obtain sufficient fiber strength for the increased amount of fibers used.
  • the fiber strength generation rate in the helical layer in order to act the force against the tank internal pressure
  • the degree to which the strength of the fiber is generated is effectively improved. In such a case, it is possible to reduce the amount of fiber used while realizing a high fiber strength occurrence rate, and to prevent the tank from becoming larger (larger).
  • the FRP layer can be made thinner and the volume of the tank can be increased.
  • the coverage by the helical layer is continuously reduced. Or it is also preferable that the coverage by a helical layer is decreasing in steps.
  • the rate of decrease in the coverage rate may be constant. Alternatively, the rate of decrease in the coverage rate may change midway.
  • the manufacturing method according to the present invention is a method for manufacturing a tank having a liner and an FRP layer comprising a hoop layer and a helical layer formed by winding fibers on the outer periphery of the liner.
  • the coverage of the tank body by the helical layer is made lower on the outer layer side than on the inner layer side of the FRP layer.
  • the present invention it is an object to provide a tank and a method for manufacturing the same in which the physique or mass of the tank is prevented from being increased by fibers such as a helical layer.
  • FIG. 1 to 9 show an embodiment of a tank and a manufacturing method thereof according to the present invention. Below, it demonstrates, exemplifying the case where the tank (high pressure tank) 1 concerning this invention is applied to the high pressure hydrogen tank as a hydrogen fuel supply source.
  • the hydrogen tank can be used in a fuel cell system or the like.
  • the tank 1 includes, for example, a cylindrical tank body 10 having both ends substantially hemispherical, and a base 11 attached to one end of the tank body 10 in the longitudinal direction.
  • the substantially hemispherical portion is referred to as a dome portion
  • the cylindrical body portion is referred to as a straight portion, which are denoted by reference numerals 1d and 1s, respectively (see FIGS. 1 and 2).
  • the tank 1 shown in this embodiment has the caps 11 at both ends, for the sake of convenience of explanation, the forward direction of the X axis (direction indicated by the arrow) in FIG. The side and the negative direction will be described as the base end side.
  • the positive direction (the direction indicated by the arrow) of the Y axis perpendicular to the X axis indicates the tank outer peripheral side.
  • the tank body 10 has, for example, a two-layer wall layer, and has a liner 20 that is an inner wall layer and, for example, an FRP layer 21 that is a resin fiber layer (reinforcing layer) that is an outer wall layer on the outer side.
  • the FRP layer 21 is formed of, for example, only the CFRP layer 21c, or the CFRP layer 21c and the GFRP layer 21g (see FIG. 1).
  • the liner 20 is formed in substantially the same shape as the tank body 10.
  • the liner 20 is made of, for example, polyethylene resin, polypropylene resin, or other hard resin.
  • the liner 20 may be a metal liner formed of aluminum or the like.
  • a folded portion 30 that is bent inward is formed on the tip end side of the liner 20 having the base 11.
  • the folded portion 30 is folded toward the inside of the tank body 10 so as to be separated from the outer FRP layer 21.
  • the folded portion 30 has, for example, a reduced diameter portion 30a that gradually decreases in diameter as it approaches the folded tip, and a cylindrical portion 30b that is connected to the distal end of the reduced diameter portion 30a and has a constant diameter.
  • the cylindrical portion 30b forms an opening of the liner 20.
  • the base 11 has a substantially cylindrical shape and is fitted into the opening of the liner 20.
  • the base 11 is made of, for example, aluminum or an aluminum alloy, and is manufactured in a predetermined shape by, for example, a die casting method.
  • the base 11 is fitted into an injection-molded split liner. Further, the base 11 may be attached to the liner 20 by insert molding, for example.
  • the base 11 has a valve fastening seat surface 11a formed on the tip side (outside in the axial direction of the high pressure tank 1), for example, and on the rear side (inside in the axial direction of the high pressure tank 1) of the valve fastening seat surface 11a.
  • An annular recess 11 b is formed with respect to the axis of the high-pressure tank 1.
  • the dent 11b is convexly curved on the shaft side and has an R shape.
  • the vicinity of the tip of the R-shaped FRP layer 21 is in airtight contact with the recess 11b.
  • the surface of the recess 11b that contacts the FRP layer 21 is provided with a solid lubricating coating C such as a fluorine-based resin. Thereby, the friction coefficient between the FRP layer 21 and the recessed part 11b is reduced.
  • the rear side of the recessed portion 11b of the base 11 is formed to fit, for example, the shape of the folded portion 30 of the liner 20, and for example, a flange portion (crest portion) 11c having a large diameter is formed continuously from the recessed portion 11b.
  • a cap cylindrical portion 11d having a constant diameter is formed rearward from the flange portion 11c.
  • the reduced diameter portion 30a of the folded portion 30 of the liner 20 is in close contact with the surface of the flange portion 11c, and the cylindrical portion 30b is in close contact with the surface of the cap cylindrical portion 11d. Seal members 40 and 41 are interposed between the cylindrical portion 30b and the base cylindrical portion 11d.
  • the valve assembly 50 controls the supply and discharge of the fuel gas between the external gas supply line (supply path 22) and the inside of the tank 1. Seal members 60 and 61 are interposed between the outer peripheral surface of the bubble assembly 50 and the inner peripheral surface of the base 11.
  • the FRP layer 21 is formed by, for example, FW molding (filament winding molding), winding a resin-impregnated fiber (reinforcing fiber) 70 around the outer peripheral surface of the liner 20 and the recess 11b of the base 11 and curing the resin.
  • FW molding filament winding molding
  • resin-impregnated fiber (reinforcing fiber) 70 around the outer peripheral surface of the liner 20 and the recess 11b of the base 11 and curing the resin.
  • the resin of the FRP layer 21 for example, an epoxy resin, a modified epoxy resin, an unsaturated polyester resin, or the like is used.
  • the fiber 70 carbon fiber (CF), metal fiber, or the like is used.
  • the outer periphery of the liner 20 is moved by moving the guide of the fiber 70 along the tank axis direction while rotating the liner 20 around the tank axis (indicated by reference numeral 12 in FIGS.
  • the fiber 70 can be wound around.
  • a fiber bundle in which a plurality of fibers 70 are bundled is generally wound around the liner 20.
  • the fiber bundle is simply referred to as a fiber including the case of a fiber bundle.
  • the FW device 80 shown in FIGS. 8 and 9 reciprocates the guide device (referred to as “eye opening”) 81 of the fiber 70 along the tank axial direction while rotating the liner 20 around the tank shaft 12.
  • the fiber 70 is wound around the outer periphery of the liner 20.
  • the winding angle of the fiber 70 can be changed by changing the relative speed of the movement of the guide device 81 with respect to the rotational speed of the liner 20.
  • the guide device 81 is operably supported by a jig, for example.
  • the tank 1 is formed by winding a fiber (for example, carbon fiber) 70 around the outer periphery of the liner 20 and curing the resin.
  • a fiber for example, carbon fiber
  • the low-angle helical layer 70HL) is formed.
  • the fiber 70 is wound around the straight portion (tank body portion) 1 s of the tank 1 like a coil spring to tighten the portion, and the force in the positive direction of the Y axis by the gas pressure (outward in the radial direction) A force to counteract the force to spread) is applied to the liner 20.
  • the latter helical winding is a winding method whose main purpose is to fasten the dome portion 1d, and the fiber 70 is entirely wound around the tank 1 so as to be caught by the dome portion 1d. This contributes to improving the strength of the portion 1d.
  • an acute angle (of which an acute angle is formed) between a string 70 of a fiber 70 wound like a coil spring (a thread line in a screw) and a center line of the tank 1 (tank shaft 12). 2) is the “winding angle with respect to the tank shaft (12)” of the fiber 70 referred to in the present specification, which is indicated by the symbol ⁇ in FIG.
  • the hoop winding is a method in which the fiber 70 is wound substantially perpendicularly to the tank shaft 12 in the straight portion, and a specific winding angle at that time is, for example, 80 to 90 ° (see FIG. 2). ).
  • Helical winding (or impeller winding) is a winding method in which the fibers 70 are wound around the dome portion, and the winding angle with respect to the tank shaft 12 is smaller than that in the case of hoop winding (see FIG. 2). If the helical winding is roughly divided into two types, there are two types: high angle helical winding and low angle helical winding.
  • the high angle helical winding has a relatively large winding angle with respect to the tank shaft 12, and specific examples of the winding angle are as follows. 70 to 80 °.
  • the low-angle helical winding has a relatively small winding angle with respect to the tank shaft 12, and a specific example of the winding angle is 5 to 30 °.
  • the winding angle when the fiber 70 is parallel to the tank shaft 12 is 0 °
  • the winding angle when the fiber 70 is wound around in the circumferential direction is 90 °.
  • the term “low angle helical winding” including helical winding at a winding angle of 0 to 5 ° is referred to.
  • a helical winding at a winding angle of 30 to 70 ° between them may be referred to as a medium angle helical winding.
  • the helical layers formed by the high angle helical winding, the medium angle helical winding, and the low angle helical winding are respectively a high angle helical layer (indicated by reference numeral 70HH), a medium angle helical layer (see FIG. 2), and a low angle helical layer ( This is indicated as 70LH.
  • the folded portion in the tank axial direction in the dome portion 1d of the high angle helical winding is referred to as a folded portion (see FIG. 2).
  • the hoop winding is a winding method that allows the fibers 70 to be wound spirally while adjoining the fibers 70 so that the fibers 70 are not stacked and the unevenness is not generated.
  • the helical winding is generally intended to tighten the dome portion, and it is difficult to reduce the stacking and unevenness of the fibers 70, or sufficient consideration is given to reducing them. There is no winding method.
  • the hoop winding and the helical winding are appropriately combined according to specifications such as the axial length and diameter of the tank 1, and the hoop layer 70P and the helical layer 70H are stacked around the liner 20 (see FIG. 1 and the like).
  • the fiber layer in the helical layer 70H is configured such that the coverage rate by the helical layer 70H with respect to the straight portion (body portion) 1s of the tank 1 is increased toward the inner layer side and gradually decreased toward the outer layer side. The strength generation rate is effectively improved (see FIG. 4 and the like).
  • the fiber 70 that is wound on the outer layer side is particularly concerned. It is difficult to sufficiently exert the strength of the FRP layer 21 with respect to the fiber strength occurrence rate, and as a result, the physique and mass of the tank 1 may increase (FIG. 9). reference).
  • the coverage ratio of the helical layer 70H with respect to the straight portion 1s is increased toward the tank inner layer side (lowered from the tank inner layer side toward the outer layer side) ( (See FIG. 4).
  • the fiber strength occurrence rate in the helical layer 70H can be effectively improved, and as a result, the physique or mass of the tank 1 can be prevented from becoming too large while ensuring the fiber strength occurrence rate. That is, in the present embodiment, the cover rate is optimized so that the FRP layer 21 can be formed thinner than the conventional one while ensuring the fiber strength generation rate (see FIG. 5). It is possible to reduce the size of the entire tank while maintaining (internal capacity), and it is possible to suppress an increase in physique without obtaining sufficient fiber strength (so-called enlargement of the tank 1). . This is particularly effective under the current situation where the tank 1 is required to have a larger size, a higher pressure, and a reduced number of tanks. Further, when the tank 1 is used as, for example, a hydrogen supply tank for a fuel cell vehicle, it can contribute to extending the cruising distance of the vehicle.
  • the aspect of the change in the coverage by the fibers 70 is not particularly limited, and may be gradually reduced from the inner layer to the outer layer of the FRP layer 21 (see FIG. 6) or stepwise. It may be decreased (see FIG. 7). Further, the rate of decrease is not particularly limited, and may be a constant rate or may be changed in the middle. Further, there is no particular limitation as to how much the coverage in the outermost helical layer 70H is to be made.
  • the cover ratio is 50% (as an example, the case where the one-side surface area of the wound fiber 70 and the gap between the fibers 70 are substantially equal as in this embodiment) is exemplified (The cover rate in the outermost layer may be higher or lower than this, and the layer having a cover rate of 50% may be used as an intermediate layer instead of the outermost layer.
  • the fibers 70 are evenly wound in one helical layer 70H (see FIG. 4). By winding so that the intervals between the fibers 70 are equal, the fiber strength generation rate by the fibers 70 can be made more uniform.
  • the fiber 70 is wound so that the covering ratio of the helical layer 70H to the straight portion 1s of the tank 1 with respect to the straight portion 1s of the tank 1 is lower on the outer layer side than the inner layer side of the FRP layer 21, and the fiber strength generation rate is more effective. Therefore, the use efficiency of the fiber 70 is improved. Moreover, it can suppress that the physique or mass of the tank 1 becomes large by this.
  • the present invention can be applied to things other than a tank (pressure vessel), for example, a cylinder (including a cylindrical part) such as a long object or a structure having an FRP layer.
  • a tank pressure vessel
  • a cylinder including a cylindrical part
  • FRP layer 21 having the helical layer 70H or the hoop layer 70P is formed by wrapping the fiber 70 around a mandrel (such as a mandrel) or a mold by helical winding or hoop winding, a hoop layer is formed.
  • the fiber strength of the fiber strength is improved by, for example, arranging 70P on the inner side to form an inner layer, or arranging the fiber folded end portion 70e so as to draw a trajectory that is narrowed toward the outer layer (defined as a set of all points satisfying a certain condition). It is possible to achieve the same operational effects as in the above-described embodiment, such as improving the expression efficiency.
  • Specific examples of the cylinder in the case where the present invention is applied to the cylinder as described above include exercise equipment such as a golf club shaft and carbon bat, leisure equipment such as a fishing rod, engineering products such as plant equipment, and building materials. Can be mentioned.
  • the helical layer 70H is a smooth helical layer to reduce unevenness that may occur in the hoop layer 70P adjacent to the outside.
  • the smooth helical layer 70 ⁇ / b> H is a layer formed by helical winding so as to reduce the overlap of the fibers 70 in the layer, and in principle, the next fiber 70 is aligned next to the adjacent fibers 70. Is wound, and the way the fibers 70 overlap is different from the conventional helical layer (uneven helical layer).
  • the fibers 70 in the hoop layer 70P are formed. Structural bending (undulations) or undulations and undulations can be reduced. That is, since the surface (surface layer) of the smooth helical layer 70H is smoother than the conventional surface, in the hoop layer 70P formed on the smooth surface, the bending (undulation) of the structural fibers 70 caused by unevenness. ) Is reduced.
  • Vf fiber volume
  • the winding start of the liner 20 can be either the fiber 70 forming the helical layer 70H or the fiber 70 forming the hoop layer 70P. In this way, by appropriately changing the fiber 70 at the start of winding, it is possible to set the break start position when the tank 1 should break. As described above, both the helical layer 70H and the hoop layer 70P have a greater contribution to the tank strength as the layer located on the inner side (the layer closer to the liner 20).
  • the break start position becomes the dome portion 1d in advance. It is possible to set.
  • the present invention is suitable when applied to a tank having an FRP layer, and further to a cylindrical body such as a long object or a structure.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

The objective is to provide a tank and a fabrication method thereof that keep the physical constitution or mass of a tank from being increased by fiber layers, such as helical layers. To realize this, a tank (1) comprises a liner (20) and an FRP layer (21), which is made from hoop layers (70P) and helical layers (70H) that are formed by fiber bundles (70) being wrapped around the outer circumference of said liner (20). The percentage of the body part (1s) of the tank (1) covered by the fibers (70) of helical layers (70H) is made lower in the outer layers than in the inner layers of the FRP layer (21). It is preferable that the percentage of coverage by helical layers (70H) decreases continuously. Alternatively, it is preferable that the percentage of coverage by helical layers (70H) decreases in a stepwise fashion.

Description

タンクおよびその製造方法Tank and manufacturing method thereof

 本発明は、タンクおよびその製造方法に関する。さらに詳述すると、本発明は、水素ガス等が高圧で充填されるタンクにおける構造の改良に関する。 The present invention relates to a tank and a manufacturing method thereof. More specifically, the present invention relates to an improvement in the structure of a tank filled with hydrogen gas or the like at a high pressure.

 水素ガス等の貯蔵に利用されるタンクとして、ライナの外周に複数のフープ層とヘリカル層とが積層されたFRP層を備え、軽量化を図ったものが利用されている(例えば特許文献1参照)。ライナは、水素ガス等の透過を防いで気密に貯蔵する部材として機能し、FRP層は、高い内圧に耐える強度を付与する部材として機能する。 As a tank used for storing hydrogen gas or the like, a tank that is provided with an FRP layer in which a plurality of hoop layers and a helical layer are laminated on the outer periphery of the liner and is reduced in weight is used (for example, see Patent Document 1). ). The liner functions as a member that prevents permeation of hydrogen gas and the like and stores it in an airtight manner, and the FRP layer functions as a member that provides strength to withstand high internal pressure.

 FRP層を形成するフープ層は、繊維(例えば炭素繊維)がフープ巻(タンク胴体部においてタンク軸にほぼ垂直に巻く巻き方)されて形成された層であり、ヘリカル層は、繊維がヘリカル巻(タンク軸にほぼ平行であり、タンクドーム部まで巻く巻き方)されて形成された層である(図2参照)。また、ヘリカル巻は、タンク軸に対する巻角度を変えることによって高角度ヘリカル巻や低角度ヘリカル巻といった態様の異なる巻き方とすることが可能である。このようにしてFRP層を形成する際、繊維をどのように巻回させるかは、FRP層による強度発現の効率を向上させるための重要な要素となっている。 The hoop layer forming the FRP layer is a layer formed by winding a fiber (for example, carbon fiber) by hoop winding (a method of winding the fiber around the tank axis in the tank body portion). (It is substantially parallel to the tank axis and is wound up to the tank dome.) (See FIG. 2). Further, helical winding can be performed in different manners such as high angle helical winding and low angle helical winding by changing the winding angle with respect to the tank axis. When forming the FRP layer in this manner, how the fibers are wound is an important factor for improving the efficiency of strength expression by the FRP layer.

 従来、繊維の具体的な巻回のさせ方としては、例えば周方向繊維層(フープ層、高角度ヘリカル層)および軸方向繊維層(低角度ヘリカル層)を交互に巻回していくというものがある。この場合、例えば軸方向繊維層(低角度ヘリカル層)を構成する繊維によって全表面を隙間なく覆うこととしているため、繊維によるカバー率が100%以上となっている。ここでいう繊維によるカバー率は、タンク胴体部の表面積に対する、当該層に巻回された繊維の片側表面積の割合を指しており、(当該層に巻回された繊維の表面積/胴体部表面積)×100で求めることができる。必要最小限の繊維によって胴体部の全表面積を覆った場合のカバー率は100%である。従来の手法では、繊維層を積層させる際にすべてのヘリカル層においてカバー率100%以上となるように繊維を巻回していることが一般的である。ちなみに、タンクは例えば円筒形状である本体部分の両端が略半球状のドーム部に形成された密閉容器であり、本明細書では略半球状部分をドーム部、筒状の胴体部分を胴体部(またはストレート部)という。 Conventionally, as a specific method of winding fibers, for example, a circumferential fiber layer (hoop layer, high-angle helical layer) and an axial fiber layer (low-angle helical layer) are alternately wound. is there. In this case, for example, since the entire surface is covered with the fibers constituting the axial fiber layer (low-angle helical layer) without any gap, the fiber coverage is 100% or more. The fiber coverage here refers to the ratio of the one-sided surface area of the fiber wound around the layer to the surface area of the tank body part (surface area of the fiber wound around the layer / body part surface area). It can be determined by x100. The coverage when the entire surface area of the body portion is covered with the minimum necessary fibers is 100%. In the conventional technique, when the fiber layers are laminated, the fibers are generally wound so that the covering ratio is 100% or more in all the helical layers. Incidentally, the tank is a sealed container in which, for example, both ends of a cylindrical main body part are formed in a substantially hemispherical dome part. In this specification, a substantially hemispherical part is a dome part, and a cylindrical body part is a body part ( Or straight part).

特開2008-032088号公報JP 2008-032088 A

 しかしながら、上述のごとき従来のタンクにおいては、外層側に積層されるヘリカル層などの繊維層により当該タンクの体格および質量が大きくなっているという点で問題である。 However, in the conventional tank as described above, there is a problem in that the size and mass of the tank are increased by a fiber layer such as a helical layer laminated on the outer layer side.

 そこで、本発明は、ヘリカル層などの繊維層によってタンクの体格または質量が大きくなるのを抑制したタンクおよびその製造方法を提供することを目的とする。 Therefore, an object of the present invention is to provide a tank that suppresses an increase in the size or mass of the tank due to a fiber layer such as a helical layer, and a manufacturing method thereof.

 かかる課題を解決するべく本発明者は種々の検討を行った。上述したように、ライナの周囲に周方向繊維層(フープ層、高角度ヘリカル層)および軸方向繊維層(低角度ヘリカル層)を巻回して繊維層を形成していくのが一般的な手法となっているが、このように繊維層を積層した場合、外側の繊維層ほど、当該繊維が備えている強度を十分に発揮することが難しくなっていると考えられる。また、強度が十分に発揮されないままに繊維が巻回されれば、強度の割に繊維量が多く、体格等の大きなタンクになってしまう場合がある。特に、外層側に巻回される繊維は、強度に対する寄与の大きさが小さいにもかかわらず、何回も巻回されればタンク大径化を招く一因になりうる。 The present inventor has made various studies to solve such problems. As described above, a general method is to form a fiber layer by winding a circumferential fiber layer (hoop layer, high-angle helical layer) and an axial fiber layer (low-angle helical layer) around the liner. However, when the fiber layers are laminated in this way, it is considered that the outer fiber layers are more difficult to fully exhibit the strength of the fibers. Further, if the fibers are wound without sufficiently exerting the strength, the amount of fibers is large for the strength, and the tank may have a large physique. In particular, the fiber wound on the outer layer side can contribute to an increase in the tank diameter if it is wound many times even though the contribution to the strength is small.

 このような状況をふまえてさらに検討を重ねた本発明者は、かかる課題の解決に結び付く新たな知見を得るに至った。本発明はかかる知見に基づくもので、ライナと、該ライナの外周に繊維が巻回されて形成されるフープ層およびヘリカル層からなるFRP層と、を有するタンクであって、ヘリカル層の繊維による当該タンクの胴体部に対するカバー率が、FRP層の内層側よりも外層側のほうで低い、というものである。 The present inventor who has further studied based on such a situation has come to obtain new knowledge that leads to the solution of such problems. The present invention is based on such knowledge, and is a tank having a liner, and a FRP layer composed of a hoop layer and a helical layer formed by winding fibers on the outer periphery of the liner, and depends on the fibers of the helical layer. The cover rate of the tank body is lower on the outer layer side than on the inner layer side of the FRP layer.

 タンクの外層側に位置する層およびヘリカル層は、タンクの筒状の胴体部(タンク胴体部)に対する繊維強度という点での寄与度が小さい。つまり、外層側に位置する繊維層ほど、あるいはより低角度のヘリカル層ほど、当該繊維が備えている強度を十分に発揮してタンクの胴体部を強く巻き締める力を作用させることが難しくなる。その一方で、筒状の胴体部におけるヘリカル層によれば、ヘリカル層などよりも大きな繊維強度を発揮することが可能である。それにもかかわらず、従来手法のように繊維によるカバー率を一律としていることは、繊維の使用量が嵩む割には十分な繊維強度が得難いという点で不利である。この点、本発明にかかるタンクにおいては、このヘリカル層による胴体部に対するカバー率を内層側ほど高くすることにより、当該ヘリカル層での繊維強度発生率(タンク内圧に抗する力を作用させるため当該繊維が備えている強度をどの程度生じさせているかの度合)を効果的に向上させることとしている。こうした場合には、高い繊維強度発生率を実現させつつ繊維の使用量を少なくし、タンクの体格が大型化(肥大化)するのを抑えることが可能である。 The layer located on the outer layer side of the tank and the helical layer have a small contribution in terms of fiber strength with respect to the cylindrical body part (tank body part) of the tank. That is, the fiber layer located on the outer layer side or the helical layer at a lower angle is more difficult to exert the strength of the fiber and to tightly wind the body portion of the tank. On the other hand, according to the helical layer in the cylindrical body part, it is possible to exert a fiber strength greater than that of the helical layer. Nevertheless, the uniform coverage by the fibers as in the conventional method is disadvantageous in that it is difficult to obtain sufficient fiber strength for the increased amount of fibers used. In this respect, in the tank according to the present invention, by increasing the coverage of the body portion by the helical layer toward the inner layer side, the fiber strength generation rate in the helical layer (in order to act the force against the tank internal pressure) The degree to which the strength of the fiber is generated is effectively improved. In such a case, it is possible to reduce the amount of fiber used while realizing a high fiber strength occurrence rate, and to prevent the tank from becoming larger (larger).

 また、このように高い繊維強度発生率を実現させつつ繊維の使用量を少なくすることができれば、FRP層をより薄くし、当該タンクの容積を拡大させることが可能となる。あるいは、容積を維持しつつタンク全体の小径化を図ることも可能となる。 Also, if the amount of fiber used can be reduced while realizing a high fiber strength occurrence rate, the FRP layer can be made thinner and the volume of the tank can be increased. Alternatively, it is possible to reduce the diameter of the entire tank while maintaining the volume.

 上述したタンクにおいては、ヘリカル層によるカバー率が連続的に減少していることが好ましい。あるいは、ヘリカル層によるカバー率が段階的に減少していることも好ましい。 In the tank described above, it is preferable that the coverage by the helical layer is continuously reduced. Or it is also preferable that the coverage by a helical layer is decreasing in steps.

 また、上述したタンクにおいて、カバー率の減少の割合が一定であってもよい。あるいは、カバー率の減少の割合が途中で変化するものであってもよい。 Further, in the above-described tank, the rate of decrease in the coverage rate may be constant. Alternatively, the rate of decrease in the coverage rate may change midway.

 また、本発明にかかる製造方法は、ライナと、該ライナの外周に繊維が巻回されて形成されるフープ層およびヘリカル層からなるFRP層と、を有するタンクの製造方法において、繊維を巻回させる際、ヘリカル層による当該タンクの胴体部に対するカバー率を、FRP層の内層側よりも外層側のほうで低くする、というものである。 The manufacturing method according to the present invention is a method for manufacturing a tank having a liner and an FRP layer comprising a hoop layer and a helical layer formed by winding fibers on the outer periphery of the liner. When this is done, the coverage of the tank body by the helical layer is made lower on the outer layer side than on the inner layer side of the FRP layer.

 本発明によれば、ヘリカル層などの繊維によってタンクの体格または質量が大きくなるのを抑制したタンクおよびその製造方法を提供することを目的とする。 According to the present invention, it is an object to provide a tank and a method for manufacturing the same in which the physique or mass of the tank is prevented from being increased by fibers such as a helical layer.

本発明の一実施形態におけるタンクの構造を示す断面図および部分拡大図である。It is sectional drawing and the elements on larger scale which show the structure of the tank in one Embodiment of this invention. 繊維の各種の巻き方について説明するための図である。It is a figure for demonstrating the various winding methods of a fiber. タンクの口金付近の構造例を示す断面図である。It is sectional drawing which shows the structural example vicinity of the nozzle | cap | die of a tank. 本発明の一実施形態におけるヘリカル層の巻回の様子を概略的に示す図である。It is a figure which shows roughly the mode of winding of the helical layer in one Embodiment of this invention. 図4に示すタンクの口金付近の断面図である。It is sectional drawing of the nozzle | cap | die vicinity of the tank shown in FIG. ヘリカル層の繊維によるカバー率を連続的に減少させる場合の一例を示すグラフである。It is a graph which shows an example in the case of decreasing continuously the coverage with the fiber of a helical layer. ヘリカル層の繊維によるカバー率を段階的に減少させる場合の一例を示すグラフである。It is a graph which shows an example in the case of decreasing the coverage by the fiber of a helical layer in steps. FW(フィラメントワインディング)装置の一例を示す図である。It is a figure which shows an example of FW (filament winding) apparatus. FW装置の繊維ガイド装置を使ってライナの外周に繊維を巻き付ける様子を示す図である。It is a figure which shows a mode that a fiber is wound around the outer periphery of a liner using the fiber guide apparatus of FW apparatus. 従来のタンクにおけるヘリカル層の巻回の様子を参考として示す図である。It is a figure which shows the mode of winding of the helical layer in the conventional tank for reference. 図10に示すタンクの口金付近の断面図である。It is sectional drawing of the nozzle | cap | die of the tank shown in FIG.

 以下、本発明の構成を図面に示す実施の形態の一例に基づいて詳細に説明する。 Hereinafter, the configuration of the present invention will be described in detail based on an example of an embodiment shown in the drawings.

 図1~図9に本発明にかかるタンクおよびその製造方法の実施形態を示す。以下では、本発明にかかるタンク(高圧タンク)1を水素燃料供給源としての高圧水素タンクに適用した場合を例示しつつ説明する。水素タンクは、燃料電池システム等において利用可能なものである。 1 to 9 show an embodiment of a tank and a manufacturing method thereof according to the present invention. Below, it demonstrates, exemplifying the case where the tank (high pressure tank) 1 concerning this invention is applied to the high pressure hydrogen tank as a hydrogen fuel supply source. The hydrogen tank can be used in a fuel cell system or the like.

 タンク1は、例えば両端が略半球状である円筒形状のタンク本体10と、当該タンク本体10の長手方向の一端部に取り付けられた口金11を有する。なお、本明細書では略半球状部分をドーム部、筒状胴体部分をストレート部といい、それぞれ符号1d,1sで表す(図1、図2等参照)。また、本実施形態で示すタンク1は両端に口金11を有するものであるが、説明の便宜上、当該タンク1の要部を示す図3中のX軸の正方向(矢示する方向)を先端側、負方向を基端側として説明を行う。このX軸に垂直なY軸の正方向(矢示する方向)がタンク外周側を指している。 The tank 1 includes, for example, a cylindrical tank body 10 having both ends substantially hemispherical, and a base 11 attached to one end of the tank body 10 in the longitudinal direction. In the present specification, the substantially hemispherical portion is referred to as a dome portion, and the cylindrical body portion is referred to as a straight portion, which are denoted by reference numerals 1d and 1s, respectively (see FIGS. 1 and 2). Moreover, although the tank 1 shown in this embodiment has the caps 11 at both ends, for the sake of convenience of explanation, the forward direction of the X axis (direction indicated by the arrow) in FIG. The side and the negative direction will be described as the base end side. The positive direction (the direction indicated by the arrow) of the Y axis perpendicular to the X axis indicates the tank outer peripheral side.

 タンク本体10は、例えば二層構造の壁層を有し、内壁層であるライナ20とその外側の外壁層である樹脂繊維層(補強層)としての例えばFRP層21を有している。FRP層21は、例えばCFRP層21cのみ、あるいは該CFRP層21cおよびGFRP層21gによって形成されている(図1参照)。 The tank body 10 has, for example, a two-layer wall layer, and has a liner 20 that is an inner wall layer and, for example, an FRP layer 21 that is a resin fiber layer (reinforcing layer) that is an outer wall layer on the outer side. The FRP layer 21 is formed of, for example, only the CFRP layer 21c, or the CFRP layer 21c and the GFRP layer 21g (see FIG. 1).

 ライナ20は、タンク本体10とほぼ同じ形状に形成される。ライナ20は、例えばポリエチレン樹脂、ポリプロピレン樹脂、またはその他の硬質樹脂などにより形成されている。あるいは、ライナ20はアルミニウムなどで形成された金属ライナであってもよい。 The liner 20 is formed in substantially the same shape as the tank body 10. The liner 20 is made of, for example, polyethylene resin, polypropylene resin, or other hard resin. Alternatively, the liner 20 may be a metal liner formed of aluminum or the like.

 ライナ20の口金11のある先端側には、内側に屈曲した折返し部30が形成されている。折返し部30は、外側のFRP層21から離間するようにタンク本体10の内側に向けて折り返されている。折返し部30は、例えば折り返しの先端に近づくにつれて次第に径が小さくなる縮径部30aと、当該縮径部30aの先端に接続され径が一定の円筒部30bとを有している。この円筒部30bによりライナ20の開口部が形成されている。 A folded portion 30 that is bent inward is formed on the tip end side of the liner 20 having the base 11. The folded portion 30 is folded toward the inside of the tank body 10 so as to be separated from the outer FRP layer 21. The folded portion 30 has, for example, a reduced diameter portion 30a that gradually decreases in diameter as it approaches the folded tip, and a cylindrical portion 30b that is connected to the distal end of the reduced diameter portion 30a and has a constant diameter. The cylindrical portion 30b forms an opening of the liner 20.

 口金11は、略円筒形状を有し、ライナ20の開口部に嵌入されている。口金11は、例えばアルミニウム又はアルミニウム合金からなり、例えばダイキャスト法等により所定の形状に製造されている。口金11は射出成形された分割ライナに嵌め込まれている。また、口金11は例えばインサート成形によりライナ20に取り付けられてもよい。 The base 11 has a substantially cylindrical shape and is fitted into the opening of the liner 20. The base 11 is made of, for example, aluminum or an aluminum alloy, and is manufactured in a predetermined shape by, for example, a die casting method. The base 11 is fitted into an injection-molded split liner. Further, the base 11 may be attached to the liner 20 by insert molding, for example.

 また、口金11は、例えば先端側(高圧タンク1の軸方向の外側)にバルブ締結座面11aが形成され、そのバルブ締結座面11aの後方側(高圧タンク1の軸方向の内側)に、高圧タンク1の軸に対して環状の凹み部11bが形成されている。凹み部11bは、軸側に凸に湾曲しR形状になっている。この凹み部11bには、同じくR形状のFRP層21の先端部付近が気密に接触している。 In addition, the base 11 has a valve fastening seat surface 11a formed on the tip side (outside in the axial direction of the high pressure tank 1), for example, and on the rear side (inside in the axial direction of the high pressure tank 1) of the valve fastening seat surface 11a. An annular recess 11 b is formed with respect to the axis of the high-pressure tank 1. The dent 11b is convexly curved on the shaft side and has an R shape. Similarly, the vicinity of the tip of the R-shaped FRP layer 21 is in airtight contact with the recess 11b.

 例えばFRP層21と接触する凹み部11bの表面には、例えばフッ素系の樹脂などの固体潤滑コーティングCが施されている。これにより、FRP層21と凹み部11bとの間の摩擦係数が低減されている。 For example, the surface of the recess 11b that contacts the FRP layer 21 is provided with a solid lubricating coating C such as a fluorine-based resin. Thereby, the friction coefficient between the FRP layer 21 and the recessed part 11b is reduced.

 口金11の凹み部11bのさらに後方側は、例えばライナ20の折返し部30の形状に適合するように形成され、例えば凹み部11bに連続して径の大きい鍔部(ツバ部)11cが形成され、その鍔部11cから後方に一定径の口金円筒部11dが形成されている。上記ライナ20の折返し部30の縮径部30aは、鍔部11cの表面に密着し、円筒部30bは、口金円筒部11dの表面に密着している。円筒部30bと口金円筒部11dとの間には、シール部材40、41が介在している。 The rear side of the recessed portion 11b of the base 11 is formed to fit, for example, the shape of the folded portion 30 of the liner 20, and for example, a flange portion (crest portion) 11c having a large diameter is formed continuously from the recessed portion 11b. A cap cylindrical portion 11d having a constant diameter is formed rearward from the flange portion 11c. The reduced diameter portion 30a of the folded portion 30 of the liner 20 is in close contact with the surface of the flange portion 11c, and the cylindrical portion 30b is in close contact with the surface of the cap cylindrical portion 11d. Seal members 40 and 41 are interposed between the cylindrical portion 30b and the base cylindrical portion 11d.

 バルブアッセンブリ50は、外部のガス供給ライン(供給路22)とタンク1の内部との間で燃料ガスの給排を制御するものである。バブルアッセンブリ50の外周面と口金11の内周面との間には、シール部材60、61が介在されている。 The valve assembly 50 controls the supply and discharge of the fuel gas between the external gas supply line (supply path 22) and the inside of the tank 1. Seal members 60 and 61 are interposed between the outer peripheral surface of the bubble assembly 50 and the inner peripheral surface of the base 11.

 FRP層21は、例えばFW成形(フィラメントワインディング成形)により、ライナ20の外周面と口金11の凹み部11bに、樹脂を含浸した繊維(補強繊維)70を巻き付け、当該樹脂を硬化させることにより形成されている。FRP層21の樹脂には、例えばエポキシ樹脂、変性エポキシ樹脂、不飽和ポリエステル樹脂等が用いられる。また、繊維70としては、炭素繊維(CF)、金属繊維などが用いられる。FW成形の際には、タンク軸(図1、図2において符号12で示す)を中心としてライナ20を回転させながら繊維70のガイドをタンク軸方向に沿って動かすことにより当該ライナ20の外周面に繊維70を巻き付けることができる。なお、実際には複数本の繊維70が束ねられた繊維束がライナ20に巻き付けられることが一般的であるが、本明細書では繊維束である場合を含めて単に繊維と呼ぶ。 The FRP layer 21 is formed by, for example, FW molding (filament winding molding), winding a resin-impregnated fiber (reinforcing fiber) 70 around the outer peripheral surface of the liner 20 and the recess 11b of the base 11 and curing the resin. Has been. For the resin of the FRP layer 21, for example, an epoxy resin, a modified epoxy resin, an unsaturated polyester resin, or the like is used. Further, as the fiber 70, carbon fiber (CF), metal fiber, or the like is used. At the time of FW molding, the outer periphery of the liner 20 is moved by moving the guide of the fiber 70 along the tank axis direction while rotating the liner 20 around the tank axis (indicated by reference numeral 12 in FIGS. 1 and 2). The fiber 70 can be wound around. In practice, a fiber bundle in which a plurality of fibers 70 are bundled is generally wound around the liner 20. However, in this specification, the fiber bundle is simply referred to as a fiber including the case of a fiber bundle.

 次に、FRP層21の繊維層71,72における繊維70のカバー率の適正化を図ったタンク1の構造例を説明する(図4等参照)。 Next, an example of the structure of the tank 1 that optimizes the coverage of the fibers 70 in the fiber layers 71 and 72 of the FRP layer 21 will be described (see FIG. 4 and the like).

 ここで、まず繊維70を巻くためのFW(フィラメントワインディング)装置の一例を簡単に説明しておく。図8、図9に示すFW装置80は、タンク軸12を中心としてライナ20を回転させながら、繊維70のガイド装置(「アイ口」などと呼ばれる)81をタンク軸方向に沿って往復動させることにより当該ライナ20の外周に繊維70を巻き付けるものである。ライナ20の回転数に対するガイド装置81の動きの相対速度を変化させることによって繊維70の巻角度を変えることができる。ガイド装置81は、例えば治具によって動作可能に支持されている。 Here, an example of an FW (filament winding) device for winding the fiber 70 will be briefly described. The FW device 80 shown in FIGS. 8 and 9 reciprocates the guide device (referred to as “eye opening”) 81 of the fiber 70 along the tank axial direction while rotating the liner 20 around the tank shaft 12. Thus, the fiber 70 is wound around the outer periphery of the liner 20. The winding angle of the fiber 70 can be changed by changing the relative speed of the movement of the guide device 81 with respect to the rotational speed of the liner 20. The guide device 81 is operably supported by a jig, for example.

 上述したように、タンク1は、ライナ20の外周に繊維(例えば炭素繊維)70を巻き付け、樹脂を硬化させることにより形成されている。ここで、繊維70の巻き付けにはフープ巻とヘリカル巻があり(図2参照)、樹脂がフープ巻された層によってフープ層70Pが、ヘリカル巻された層によってヘリカル層70H(高角度ヘリカル層70HH、低角度ヘリカル層70HL)がそれぞれ形成される。前者のフープ巻は、タンク1のストレート部(タンク胴体部分)1sに繊維70をコイルスプリングのように巻くことによって当該部分を巻き締め、気体圧によりY軸正方向へ向かう力(径方向外側へ拡がろうとする力)に対抗するための力をライナ20に作用させるものである。一方、後者のヘリカル巻はドーム部1dを巻き締めることを主目的とした巻き方であり、当該ドーム部1dに引っ掛かるようにして繊維70をタンク1に対し全体的に巻き付けることにより、主として当該ドーム部1dの強度向上に寄与する。なお、コイルスプリングのように巻かれた繊維70の弦巻(つるまき)線(ネジにおけるネジ山の線)と、当該タンク1の中心線(タンク軸12)とのなす角度(のうちの鋭角のほう)が、図2において符号αで示す、本明細書でいう繊維70の「タンク軸(12)に対する巻角度」である(図2参照)。 As described above, the tank 1 is formed by winding a fiber (for example, carbon fiber) 70 around the outer periphery of the liner 20 and curing the resin. Here, there are a hoop winding and a helical winding for winding the fiber 70 (see FIG. 2). , The low-angle helical layer 70HL) is formed. In the former hoop winding, the fiber 70 is wound around the straight portion (tank body portion) 1 s of the tank 1 like a coil spring to tighten the portion, and the force in the positive direction of the Y axis by the gas pressure (outward in the radial direction) A force to counteract the force to spread) is applied to the liner 20. On the other hand, the latter helical winding is a winding method whose main purpose is to fasten the dome portion 1d, and the fiber 70 is entirely wound around the tank 1 so as to be caught by the dome portion 1d. This contributes to improving the strength of the portion 1d. In addition, an acute angle (of which an acute angle is formed) between a string 70 of a fiber 70 wound like a coil spring (a thread line in a screw) and a center line of the tank 1 (tank shaft 12). 2) is the “winding angle with respect to the tank shaft (12)” of the fiber 70 referred to in the present specification, which is indicated by the symbol α in FIG.

 これら種々の巻き付け方のうち、フープ巻は、ストレート部において繊維70をタンク軸12にほぼ垂直に巻くものであり、その際の具体的な巻角度は例えば80~90°である(図2参照)。ヘリカル巻(または、インプレ巻)は、ドーム部にも繊維70を巻き付ける巻き方であり、タンク軸12に対する巻角度がフープ巻の場合よりも小さい(図2参照)。ヘリカル巻を大きく2つに分ければ高角度ヘリカル巻と低角度ヘリカル巻の2種類があり、そのうち高角度ヘリカル巻はタンク軸12に対する巻角度が比較的大きいもので、その巻角度の具体例は70~80°である。一方、低角度ヘリカル巻は、タンク軸12に対する巻角度が比較的小さいもので、その巻角度の具体例は5~30°である。ちなみに、繊維70がタンク軸12と平行な場合の巻角度は0°、周方向に周回するように巻かれた場合の巻角度は90°ということになる。本実施形態では、巻角度0~5°の場合のヘリカル巻を含めて低角度ヘリカル巻と呼ぶ。 Of these various winding methods, the hoop winding is a method in which the fiber 70 is wound substantially perpendicularly to the tank shaft 12 in the straight portion, and a specific winding angle at that time is, for example, 80 to 90 ° (see FIG. 2). ). Helical winding (or impeller winding) is a winding method in which the fibers 70 are wound around the dome portion, and the winding angle with respect to the tank shaft 12 is smaller than that in the case of hoop winding (see FIG. 2). If the helical winding is roughly divided into two types, there are two types: high angle helical winding and low angle helical winding. Among them, the high angle helical winding has a relatively large winding angle with respect to the tank shaft 12, and specific examples of the winding angle are as follows. 70 to 80 °. On the other hand, the low-angle helical winding has a relatively small winding angle with respect to the tank shaft 12, and a specific example of the winding angle is 5 to 30 °. Incidentally, the winding angle when the fiber 70 is parallel to the tank shaft 12 is 0 °, and the winding angle when the fiber 70 is wound around in the circumferential direction is 90 °. In the present embodiment, the term “low angle helical winding” including helical winding at a winding angle of 0 to 5 ° is referred to.

 なお、本明細書においては、これらの間となる30~70°の巻角度でのヘリカル巻を中角度ヘリカル巻と呼ぶ場合がある。さらに、高角度ヘリカル巻、中角度ヘリカル巻、低角度ヘリカル巻により形成されるヘリカル層をそれぞれ高角度ヘリカル層(符号70HHで示す)、中角度ヘリカル層(図2参照)、低角度ヘリカル層(符号70LHで示す)と呼ぶ。また、高角度ヘリカル巻のドーム部1dにおけるタンク軸方向の折り返し部分を折返し部と呼ぶ(図2参照)。 In the present specification, a helical winding at a winding angle of 30 to 70 ° between them may be referred to as a medium angle helical winding. Further, the helical layers formed by the high angle helical winding, the medium angle helical winding, and the low angle helical winding are respectively a high angle helical layer (indicated by reference numeral 70HH), a medium angle helical layer (see FIG. 2), and a low angle helical layer ( This is indicated as 70LH. Further, the folded portion in the tank axial direction in the dome portion 1d of the high angle helical winding is referred to as a folded portion (see FIG. 2).

 一般的に、フープ巻は、それ自体、繊維70どうしを隣接させながら螺旋状に巻き、繊維70の積み重ねをなくして凹凸を生じさせないようにすることが可能な巻き方である。一方、ヘリカル巻は、一般的にはドーム部を巻き締めることを主目的としており、繊維70の積み重なりや凹凸を減らすことは困難であるか、あるいはこれらを低減させることについて十分には考慮されていない巻き方である。これらフープ巻とヘリカル巻は、当該タンク1の軸長、直径などの仕様に応じて適宜組み合わされ、ライナ20の周囲にフープ層70Pおよびヘリカル層70Hが積層される(図1等参照)。このとき、繊維70によるカバー率(タンク1のストレート部1sの表面積に対する、当該層に巻回された繊維70の片側表面積の割合)を各層において一律とすることは、繊維70の使用量が嵩む割には十分な繊維強度が得難いという点で不利である。この点、本実施形態では、タンク1のストレート部(胴体部)1sに対するヘリカル層70Hによるカバー率をタンク内層側ほど高く、外層側へ向かうにつれ徐々に低くすることにより、当該ヘリカル層70Hにおける繊維強度発生率を効果的に向上させている(図4等参照)。 In general, the hoop winding is a winding method that allows the fibers 70 to be wound spirally while adjoining the fibers 70 so that the fibers 70 are not stacked and the unevenness is not generated. On the other hand, the helical winding is generally intended to tighten the dome portion, and it is difficult to reduce the stacking and unevenness of the fibers 70, or sufficient consideration is given to reducing them. There is no winding method. The hoop winding and the helical winding are appropriately combined according to specifications such as the axial length and diameter of the tank 1, and the hoop layer 70P and the helical layer 70H are stacked around the liner 20 (see FIG. 1 and the like). At this time, making the coverage by the fibers 70 (the ratio of the one-side surface area of the fibers 70 wound around the layer to the surface area of the straight portion 1s of the tank 1) uniform in each layer increases the amount of the fibers 70 used. However, it is disadvantageous in that it is difficult to obtain sufficient fiber strength. In this respect, in the present embodiment, the fiber layer in the helical layer 70H is configured such that the coverage rate by the helical layer 70H with respect to the straight portion (body portion) 1s of the tank 1 is increased toward the inner layer side and gradually decreased toward the outer layer side. The strength generation rate is effectively improved (see FIG. 4 and the like).

 すなわち、従来のようにヘリカル層70Hにおけるカバー率を例えば一律100%あるいはそれ以上とした状態で繊維70を巻回すると(図8参照)、特に外層側に巻回される繊維70ほど当該繊維70が備える強度を十分に発揮させることが難しくなり、尚かつ、繊維強度発生率の割にFRP層21の厚みが大きく、結果としてタンク1の体格および質量が大きくなってしまうことがある(図9参照)。これに対し、本実施形態のタンク1の場合には、ストレート部1sに対するヘリカル層70Hによるカバー率を、タンク内層側ほど高くする(タンク内層側から外層側に向かうにつれて低くする)こととしている(図4参照)。こうした場合、当該ヘリカル層70Hにおける繊維強度発生率を効果的に向上させることができ、ひいては、繊維強度発生率を確保しつつタンク1の体格または質量が大きくなりすぎるのを抑えることができる。つまり、本実施形態においては、繊維強度発生率を確保しつつFRP層21を従来よりも薄く形成することができるようにカバー率を適正化しているため(図5参照)、相対的に、容積(内容量)を維持しつつタンク全体の小型化を図ることが可能となり、十分な繊維強度が得られないままに体格ばかりが大きくなること(タンク1のいわば肥大化)を抑制することができる。このことは、タンク1の大型化・高圧化やンク本数の減少化などが要請される近時の現状下では特に有効である。また、タンク1が例えば燃料電池車用の水素供給用タンクとして利用される場合には、当該車両の航続距離の延伸に寄与することができる。 That is, when the fiber 70 is wound in a state in which the cover rate in the helical layer 70H is, for example, uniformly 100% or more as in the conventional case (see FIG. 8), the fiber 70 that is wound on the outer layer side is particularly concerned. It is difficult to sufficiently exert the strength of the FRP layer 21 with respect to the fiber strength occurrence rate, and as a result, the physique and mass of the tank 1 may increase (FIG. 9). reference). On the other hand, in the case of the tank 1 of the present embodiment, the coverage ratio of the helical layer 70H with respect to the straight portion 1s is increased toward the tank inner layer side (lowered from the tank inner layer side toward the outer layer side) ( (See FIG. 4). In such a case, the fiber strength occurrence rate in the helical layer 70H can be effectively improved, and as a result, the physique or mass of the tank 1 can be prevented from becoming too large while ensuring the fiber strength occurrence rate. That is, in the present embodiment, the cover rate is optimized so that the FRP layer 21 can be formed thinner than the conventional one while ensuring the fiber strength generation rate (see FIG. 5). It is possible to reduce the size of the entire tank while maintaining (internal capacity), and it is possible to suppress an increase in physique without obtaining sufficient fiber strength (so-called enlargement of the tank 1). . This is particularly effective under the current situation where the tank 1 is required to have a larger size, a higher pressure, and a reduced number of tanks. Further, when the tank 1 is used as, for example, a hydrogen supply tank for a fuel cell vehicle, it can contribute to extending the cruising distance of the vehicle.

 ここで、繊維70によるカバー率の変化の態様は特に限定されることはなく、FRP層21の内層から外層に向かって連続的に漸次減少するものでもよいし(図6参照)、段階的に減少するものでもよい(図7参照)。また、減少の割合についても特に限定はされず、一定割合であってもよいし、減少割合が途中で変化するものであってもよい。さらに、最外層のヘリカル層70Hにおけるカバー率をどの程度にするかも特に限定されない。本実施形態ではカバー率が50%である場合(一例として、本実施形態におけるように巻回された繊維70の片側表面積と繊維70間の隙間とがほぼ等しい場合)を例示しているが(図4参照)、最外層でのカバー率がこれより高くても低くても構わないし、このカバー率50%の層を最外層ではなく途中の層としても構わない。 Here, the aspect of the change in the coverage by the fibers 70 is not particularly limited, and may be gradually reduced from the inner layer to the outer layer of the FRP layer 21 (see FIG. 6) or stepwise. It may be decreased (see FIG. 7). Further, the rate of decrease is not particularly limited, and may be a constant rate or may be changed in the middle. Further, there is no particular limitation as to how much the coverage in the outermost helical layer 70H is to be made. In this embodiment, the cover ratio is 50% (as an example, the case where the one-side surface area of the wound fiber 70 and the gap between the fibers 70 are substantially equal as in this embodiment) is exemplified ( The cover rate in the outermost layer may be higher or lower than this, and the layer having a cover rate of 50% may be used as an intermediate layer instead of the outermost layer.

 ただし上述した形態のいずれにおいても、ある一つのヘリカル層70Hの中においては繊維70が均等に巻回されていることが好ましい(図4参照)。繊維70どうしの間隔が均等となるように巻回することによって、繊維70による繊維強度発生率をより均等なものとすることができる。 However, in any of the above-described forms, it is preferable that the fibers 70 are evenly wound in one helical layer 70H (see FIG. 4). By winding so that the intervals between the fibers 70 are equal, the fiber strength generation rate by the fibers 70 can be made more uniform.

 以上説明した本実施形態のタンク1においては以下に述べるような作用効果が得られる。すなわち、ヘリカル層70Hの繊維70による当該タンク1のストレート部1sに対するカバー率がFRP層21の内層側よりも外層側のほうで低くなるように繊維70を巻回し、繊維強度発生率をより効果的なものとしているので繊維70の使用効率が向上する。また、これにより、タンク1の体格または質量が大きくなるのを抑制することができる。 In the tank 1 of the present embodiment described above, the following effects can be obtained. That is, the fiber 70 is wound so that the covering ratio of the helical layer 70H to the straight portion 1s of the tank 1 with respect to the straight portion 1s of the tank 1 is lower on the outer layer side than the inner layer side of the FRP layer 21, and the fiber strength generation rate is more effective. Therefore, the use efficiency of the fiber 70 is improved. Moreover, it can suppress that the physique or mass of the tank 1 becomes large by this.

 なお、上述の実施形態は本発明の好適な実施の一例ではあるがこれに限定されるものではなく本発明の要旨を逸脱しない範囲において種々変形実施可能である。例えば上述した実施形態では、燃料電池システム等において利用可能な水素タンクに本発明を適用した場合を例示して説明したが、水素ガス以外の流体を充填するためのタンク、例えばCNG(圧縮天然ガス)を燃料として用いるCNG車両に利用される高圧圧力容器などに対しても本発明を適用することはもちろん可能である。 The above-described embodiment is an example of a preferred embodiment of the present invention, but is not limited thereto, and various modifications can be made without departing from the gist of the present invention. For example, in the above-described embodiment, the case where the present invention is applied to a hydrogen tank that can be used in a fuel cell system or the like has been described as an example. However, a tank for filling a fluid other than hydrogen gas, for example, CNG (compressed natural gas) Of course, the present invention can also be applied to a high-pressure vessel used in a CNG vehicle that uses) as a fuel.

 さらに、本発明を、タンク(圧力容器)以外の物、例えば、FRP層を有する長尺物や構造物などの筒体(筒状の部分を含む)に適用することも可能である。一例を挙げれば、心棒(例えばマンドレルのようなもの)や型の外側にヘリカル巻やフープ巻によって繊維70を巻き付けてヘリカル層70Hやフープ層70Pを有するFRP層21を形成する場合に、フープ層70Pを内側に集約して内層化しあるいは繊維折返し端部70eを外層に向かうにつれて狭まる軌跡(ある一定条件を満たす点全体の集合などと定義される)を描くように配置するなどにより、繊維強度の発現効率を向上させるといった、上述した実施形態におけるのと同様の作用効果を実現することが可能となる。このように本発明を筒体に適用する場合における筒体の具体例としては、ゴルフクラブのシャフトやカーボンバットといった運動用具、釣竿等のレジャー用具、さらにはプラント設備等のエンジニアリング製品、建築資材などの構造物といったものを挙げることができる。 Furthermore, the present invention can be applied to things other than a tank (pressure vessel), for example, a cylinder (including a cylindrical part) such as a long object or a structure having an FRP layer. For example, when the FRP layer 21 having the helical layer 70H or the hoop layer 70P is formed by wrapping the fiber 70 around a mandrel (such as a mandrel) or a mold by helical winding or hoop winding, a hoop layer is formed. The fiber strength of the fiber strength is improved by, for example, arranging 70P on the inner side to form an inner layer, or arranging the fiber folded end portion 70e so as to draw a trajectory that is narrowed toward the outer layer (defined as a set of all points satisfying a certain condition). It is possible to achieve the same operational effects as in the above-described embodiment, such as improving the expression efficiency. Specific examples of the cylinder in the case where the present invention is applied to the cylinder as described above include exercise equipment such as a golf club shaft and carbon bat, leisure equipment such as a fishing rod, engineering products such as plant equipment, and building materials. Can be mentioned.

 また、上述した実施形態では詳述していないが、ヘリカル層70Hの少なくとも一部を平滑ヘリカル層とし、その外側に隣接するフープ層70Pに生じうる凹凸を低減させることも好ましい。ここでいう平滑ヘリカル層70Hは、当該層内における繊維70どうしの重なりを低減させるようにしたヘリカル巻によって形成される層であり、原則、隣接する繊維70の真横に並ぶように次の繊維70が巻かれており、繊維70の重なり方が従来のヘリカル層(凹凸ヘリカル層)とは異なる。このように、一部のヘリカル層70Hを平滑ヘリカル層としたうえで、当該平滑ヘリカル層70Hの外側に繊維70をフープ巻してフープ層70Pを形成した場合、当該フープ層70Pにおける繊維70の構造的な曲げ(起伏)ないしは波打ち、うねりを低減することができる。すなわち、平滑ヘリカル層70Hの表面(表層)は従来よりも平滑な面となるため、当該平滑面の上に形成されるフープ層70Pにおいては、凹凸に起因する構造的な繊維70の曲げ(起伏)が低減する。このようにフープ層70Pの繊維70の構造的な曲げ(起伏)を抑えることにより当該繊維70の疲労強度を向上させることができ、尚かつ、当該フープ層70Pが薄肉化、高Vf(繊維体積含有率)化してバースト強度が向上するという利点が得られる。また、ヘリカル層70H自体が平滑であることも、当該層の薄肉化、高Vf化を通じてバースト強度を向上させうる。Vfは繊維体積含有率を表し、その値(Vf値)が大きくなると繊維の含有率が高くなり、樹脂の含有率が小さくなる。このVfの値が高すぎると疲労耐久性が悪化し、値を下げすぎるとタンク外径が大きくなる。 Although not described in detail in the above-described embodiment, it is also preferable that at least a part of the helical layer 70H is a smooth helical layer to reduce unevenness that may occur in the hoop layer 70P adjacent to the outside. The smooth helical layer 70 </ b> H here is a layer formed by helical winding so as to reduce the overlap of the fibers 70 in the layer, and in principle, the next fiber 70 is aligned next to the adjacent fibers 70. Is wound, and the way the fibers 70 overlap is different from the conventional helical layer (uneven helical layer). As described above, when a part of the helical layer 70H is a smooth helical layer and the hoop layer 70P is formed by hooping the fibers 70 outside the smooth helical layer 70H, the fibers 70 in the hoop layer 70P are formed. Structural bending (undulations) or undulations and undulations can be reduced. That is, since the surface (surface layer) of the smooth helical layer 70H is smoother than the conventional surface, in the hoop layer 70P formed on the smooth surface, the bending (undulation) of the structural fibers 70 caused by unevenness. ) Is reduced. Thus, by suppressing the structural bending (undulation) of the fiber 70 of the hoop layer 70P, the fatigue strength of the fiber 70 can be improved, and the hoop layer 70P is thinned and has a high Vf (fiber volume). Content ratio) and the burst strength is improved. In addition, the fact that the helical layer 70H itself is smooth can improve the burst strength through thinning the layer and increasing Vf. Vf represents the fiber volume content. When the value (Vf value) increases, the fiber content increases and the resin content decreases. If the value of Vf is too high, fatigue durability deteriorates, and if the value is too low, the outer diameter of the tank increases.

 また、上述したタンク1において、ライナ20に対する巻き始めを、ヘリカル層70Hを形成する繊維70、あるいはフープ層70Pを形成する繊維70のいずれとすることも可能である。このように巻き始めの繊維70を適宜変更することにより、当該タンク1が万が一破壊に至る場合の破壊開始位置を設定することができる。上述したように、ヘリカル層70H、フープ層70Pとも、内側に位置する層(ライナ20寄りの層)ほどタンク強度への寄与度が大きい。そこで、例えば、ライナ20に対する巻き始めをフープ層70Pの形成繊維70とし、ストレート部1sに対する繊維強度をドーム部1dに対するそれよりも大きくすることにより、破壊開始位置がドーム部1dとなるように予め設定することが可能である。 In the tank 1 described above, the winding start of the liner 20 can be either the fiber 70 forming the helical layer 70H or the fiber 70 forming the hoop layer 70P. In this way, by appropriately changing the fiber 70 at the start of winding, it is possible to set the break start position when the tank 1 should break. As described above, both the helical layer 70H and the hoop layer 70P have a greater contribution to the tank strength as the layer located on the inner side (the layer closer to the liner 20). Therefore, for example, by forming the winding start with respect to the liner 20 as the forming fiber 70 of the hoop layer 70P and making the fiber strength with respect to the straight portion 1s larger than that with respect to the dome portion 1d, the break start position becomes the dome portion 1d in advance. It is possible to set.

 本発明は、FRP層を有するタンク、さらには長尺物や構造物などの筒体に適用しても好適なものである。 The present invention is suitable when applied to a tank having an FRP layer, and further to a cylindrical body such as a long object or a structure.

1…タンク、1s…ストレート部(胴体部)、20…ライナ、21…FRP層、70…繊維、70H…ヘリカル層、70P…フープ層 DESCRIPTION OF SYMBOLS 1 ... Tank, 1s ... Straight part (torso part), 20 ... Liner, 21 ... FRP layer, 70 ... Fiber, 70H ... Helical layer, 70P ... Hoop layer

Claims (6)

 ライナと、該ライナの外周に繊維が巻回されて形成されるフープ層およびヘリカル層からなるFRP層と、を有するタンクであって、
 前記ヘリカル層の前記繊維による当該タンクの胴体部に対するカバー率が、前記FRP層の内層側よりも外層側のほうで低いタンク。
A tank having a liner, and an FRP layer composed of a hoop layer and a helical layer formed by winding fibers on the outer periphery of the liner,
A tank in which the coverage of the helical layer by the fibers to the body portion of the tank is lower on the outer layer side than on the inner layer side of the FRP layer.
 前記ヘリカル層による前記カバー率が連続的に減少している、請求項1に記載のタンク。 The tank according to claim 1, wherein the coverage by the helical layer is continuously reduced.  前記ヘリカル層による前記カバー率が段階的に減少している、請求項1に記載のタンク。 The tank according to claim 1, wherein the coverage by the helical layer is decreased stepwise.  前記カバー率の減少の割合が一定である、請求項2または3に記載のタンク。 The tank according to claim 2 or 3, wherein a rate of decrease in the cover rate is constant.  前記カバー率の減少の割合が途中で変化する、請求項2または3に記載のタンク。 The tank according to claim 2 or 3, wherein a rate of decrease in the coverage rate changes midway.  ライナと、該ライナの外周に繊維が巻回されて形成されるフープ層およびヘリカル層からなるFRP層と、を有するタンクの製造方法において、
 前記繊維を巻回させる際、前記ヘリカル層による当該タンクの胴体部に対するカバー率を、前記FRP層の内層側よりも外層側のほうで低くする、タンクの製造方法。
In a method of manufacturing a tank having a liner and an FRP layer composed of a hoop layer and a helical layer formed by winding fibers on the outer periphery of the liner,
A method for manufacturing a tank, wherein when the fiber is wound, a covering ratio of the helical layer to the body portion of the tank is lower on the outer layer side than on the inner layer side of the FRP layer.
PCT/JP2009/057358 2009-04-10 2009-04-10 Tank and fabrication method thereof Ceased WO2010116529A1 (en)

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US20180290537A1 (en) * 2017-04-07 2018-10-11 Toyota Jidosha Kabushiki Kaisha Tank manufacturing method and tank
CN111438930A (en) * 2019-01-16 2020-07-24 丰田自动车株式会社 Method for manufacturing high-pressure tank
JP7001041B2 (en) 2018-11-02 2022-02-03 トヨタ自動車株式会社 Manufacturing method of high pressure tank
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Publication number Priority date Publication date Assignee Title
US20180202553A1 (en) * 2017-01-16 2018-07-19 Toyota Jidosha Kabushiki Kaisha Method for producing tank with protective member
US10907733B2 (en) * 2017-01-16 2021-02-02 Toyota Jidosha Kabushiki Kaisha Method for producing tank with protective member
US20180290537A1 (en) * 2017-04-07 2018-10-11 Toyota Jidosha Kabushiki Kaisha Tank manufacturing method and tank
JP2018179081A (en) * 2017-04-07 2018-11-15 トヨタ自動車株式会社 Tank manufacturing method and tank
US10632836B2 (en) * 2017-04-07 2020-04-28 Toyota Jidosha Kabushiki Kaisha Tank manufacturing method and tank
US20200223307A1 (en) * 2017-04-07 2020-07-16 Toyota Jidosha Kabushiki Kaisha Tank manufacturing method and tank
US11104219B2 (en) 2017-04-07 2021-08-31 Toyota Jidosha Kabushiki Kaisha Tank manufacturing method and tank
JP7001041B2 (en) 2018-11-02 2022-02-03 トヨタ自動車株式会社 Manufacturing method of high pressure tank
US11285658B2 (en) * 2018-11-02 2022-03-29 Toyota Jidosha Kabushiki Kaisha Manufacturing method for high pressure tank
CN111438930A (en) * 2019-01-16 2020-07-24 丰田自动车株式会社 Method for manufacturing high-pressure tank
US11566752B2 (en) 2020-07-31 2023-01-31 Toyota Jidosha Kabushiki Kaisha High-pressure tank and method for manufacturing high-pressure tank

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